46
14 CFR Ch. I (1–1–14 Edition)
Pt. 60, App. A
T
ABLE
A2A—F
ULL
F
LIGHT
S
IMULATOR
(FFS) O
BJECTIVE
T
ESTS
—Continued
QPS Requirements
Information
Test
Tolerance
Flight conditions
Test details
Simulator level
Notes
Entry No.
Title
A B
C
D
1.c.2.
.............
One engine Inoperative
..
±
3 kts airspeed,
±
5% or
±
100 FPM (0.5 m/Sec.)
climb rate, but not less
than the climb gradient re-
quirements of 14 CFR
part 23 or part 25, as ap-
propriate.
For part 23 airplanes,
in accordance with
part 23. For part 25
airplanes, Second
Segment Climb.
Flight test data is preferred, however,
airplane performance manual data is
an acceptable alternative. Test at
weight, altitude, or temperature limiting
conditions. Record at nominal climb
speed. Flight simulator performance
must be recorded over an interval of
at least 1,000 ft. (300 m).
X X X X
1.c.3.
.............
One Engine Inoperative
En route Climb.
±
10% time,
±
10% distance,
±
10% fuel used.
Clean
...........................
Record results for at least a 5000 ft
(1550 m) climb segment. Flight test
data or airplane performance manual
data may be used.
X X
1.c.4.
.............
One Engine Inoperative
Approach Climb (if op-
erations in icing condi-
tions are authorized).
±
3 kts airspeed,
±
5% or
±
100 FPM (0.5 m/Sec.)
climb rate, but not less
than the climb gradient re-
quirements of 14 CFR
parts 23 or 25 climb gra-
dient, as appropriate.
Approach
.....................
Record results at near maximum gross
landing weight as defined in Appendix
F of this part. Flight test data or air-
plane performance manual data may
be used. Flight simulator performance
must be recorded over an interval of
at least 1,000 ft. (300 m).
X
X
X
X
The airplane should be
configured with all
anti-ice and de-ice
systems operating
normally, with the
gear up and go-
around flaps set. All
icing accountability
considerations
should be applied in
accordance with the
aircraft certification
or authorization for
an approach in icing
conditions.
1.d.
................
Cruise/Descent.
1.d.1.
.............
Level flight acceleration
..
±
5%
Time
.............................
Cruise
..........................
Record results for a minimum of 50 kts
speed increase using maximum con-
tinuous thrust rating or equivalent.
X X X X
1.d.2.
.............
Level flight deceleration
..
±
5%
Time
.............................
Cruise
..........................
Record results for a minimum of 50 kts.
speed decrease using idle power.
X X X X
VerDate Mar<15>2010
20:48 Jan 30, 2014
Jkt 232047
PO 00000
Frm 00056
Fmt 8010
Sfmt 8002
Q:\14\14V2.TXT
ofr150
PsN: PC150